FR2781791A1 - PROCESS FOR MANUFACTURING PARTS OF COMPOSITE MATERIALS REINFORCED WITH FIBERS - Google Patents
PROCESS FOR MANUFACTURING PARTS OF COMPOSITE MATERIALS REINFORCED WITH FIBERS Download PDFInfo
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- FR2781791A1 FR2781791A1 FR9909854A FR9909854A FR2781791A1 FR 2781791 A1 FR2781791 A1 FR 2781791A1 FR 9909854 A FR9909854 A FR 9909854A FR 9909854 A FR9909854 A FR 9909854A FR 2781791 A1 FR2781791 A1 FR 2781791A1
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- silicon
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/10—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/006—Pressing and sintering powders, granules or fibres
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
- C04B35/565—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide
- C04B35/573—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide obtained by reaction sintering or recrystallisation
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/64—Burning or sintering processes
- C04B35/65—Reaction sintering of free metal- or free silicon-containing compositions
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/71—Ceramic products containing macroscopic reinforcing agents
- C04B35/78—Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
- C04B35/80—Fibres, filaments, whiskers, platelets, or the like
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/71—Ceramic products containing macroscopic reinforcing agents
- C04B35/78—Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
- C04B35/80—Fibres, filaments, whiskers, platelets, or the like
- C04B35/83—Carbon fibres in a carbon matrix
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D65/00—Parts or details
- F16D65/02—Braking members; Mounting thereof
- F16D65/12—Discs; Drums for disc brakes
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
- F16D69/02—Composition of linings ; Methods of manufacturing
- F16D69/023—Composite materials containing carbon and carbon fibres or fibres made of carbonizable material
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C43/36—Moulds for making articles of definite length, i.e. discrete articles
- B29C43/361—Moulds for making articles of definite length, i.e. discrete articles with pressing members independently movable of the parts for opening or closing the mould, e.g. movable pistons
- B29C2043/3615—Forming elements, e.g. mandrels or rams or stampers or pistons or plungers or punching devices
- B29C2043/3628—Forming elements, e.g. mandrels or rams or stampers or pistons or plungers or punching devices moving inside a barrel or container like sleeve
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C43/36—Moulds for making articles of definite length, i.e. discrete articles
- B29C2043/3665—Moulds for making articles of definite length, i.e. discrete articles cores or inserts, e.g. pins, mandrels, sliders
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C43/36—Moulds for making articles of definite length, i.e. discrete articles
- B29C2043/3665—Moulds for making articles of definite length, i.e. discrete articles cores or inserts, e.g. pins, mandrels, sliders
- B29C2043/3668—Moulds for making articles of definite length, i.e. discrete articles cores or inserts, e.g. pins, mandrels, sliders destructible or fusible
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/16—Frictional elements, e.g. brake or clutch linings
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/709—Articles shaped in a closed loop, e.g. conveyor belts
- B29L2031/7096—Rings or ring-like articles
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/60—Aspects relating to the preparation, properties or mechanical treatment of green bodies or pre-forms
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/94—Products characterised by their shape
- C04B2235/945—Products containing grooves, cuts, recesses or protusions
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D65/00—Parts or details
- F16D65/02—Braking members; Mounting thereof
- F16D2065/13—Parts or details of discs or drums
- F16D2065/1304—Structure
- F16D2065/1328—Structure internal cavities, e.g. cooling channels
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D2200/00—Materials; Production methods therefor
- F16D2200/0034—Materials; Production methods therefor non-metallic
- F16D2200/0039—Ceramics
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D2200/00—Materials; Production methods therefor
- F16D2200/006—Materials; Production methods therefor containing fibres or particles
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D2250/00—Manufacturing; Assembly
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D2250/00—Manufacturing; Assembly
- F16D2250/0007—Casting
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D2250/00—Manufacturing; Assembly
- F16D2250/0092—Tools or machines for producing linings
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Composite Materials (AREA)
- Inorganic Chemistry (AREA)
- Ceramic Products (AREA)
Abstract
a) Procédé permettant de fabriquer des pièces céramiques à structure interne et en particulier à passages internes. b) Procédé caractérisé par le fait que l'on ajoute au moins un noyau métallique (20) constitué de silicium ou d'un alliage de silicium qui est introduit à la presse dans l'ébauche et y subsiste et sert de source de silicium lors de l'infiltration par bain de fusion.c) L'invention permet en particulier de fabriquer des disques de frein en céramique autorisant une ventilation interne du disque.a) Method for manufacturing ceramic parts with internal structure and in particular with internal passages. b) A method characterized by the fact that at least one metal core (20) consisting of silicon or a silicon alloy is added which is introduced to the press in the blank and remains there and serves as a source of silicon during infiltration by a melt bath. c) The invention makes it possible in particular to manufacture ceramic brake discs allowing internal ventilation of the disc.
Description
II
PROCÉDÉ DE FABRICATION DE PIÈCES EN MATÉRIAUX METHOD FOR MANUFACTURING PARTS OF MATERIALS
COMPOSITES ARMÉS DE FIBRES.ARMORED FIBER COMPOSITES.
La présente invention concerne un procédé de fabrication de pièces en matériaux composites armés de fibres à partir de pièces brutes armées de fibres, présentant une matrice de carbone poreuse à base de carbone, en particulier à partir de pièces composites céramique/céramique C/C, dans le cas duquel on mélange des fibres, des faisceaux de matériau fibreux ou des agglomérats de fibres à base de carbone, azote, bore et/ou silicium, avec au moins un liant carbonisable et éventuellement d'autres matériaux d'addition ou charges pour obtenir une masse à presser et on presse la masse à presser pour obtenir une ébauche, que l'on pyrolyse ensuite, le liant, dont il y a au moins un, se convertissant en une matrice à base de carbone poreuse et la pièce brute, armée de fibres, résultante The present invention relates to a method for manufacturing parts made of fiber-reinforced composite materials from raw parts armed with fibers, having a porous carbon matrix based on carbon, in particular from ceramic / ceramic C / C composite parts, in the case of which fibers, bundles of fibrous material or fiber agglomerates based on carbon, nitrogen, boron and / or silicon are mixed, with at least one carbonisable binder and possibly other addition materials or fillers for obtain a mass to be pressed and the mass to be pressed is pressed to obtain a blank, which is then pyrolyzed, the binder, of which there is at least one, converting into a matrix based on porous carbon and the raw part, army of fibers, resulting
étant infiltrée d'un métal ou de silicium en fusion. being infiltrated with a molten metal or silicon.
Le procédé conforme à l'invention concerne en particulier la fabrication de matériaux céramiques composites ainsi que des matériaux céramiques composites armés de fibres. On y infiltre une pièce précéramique poreuse avec un bain de fusion d'un métal ou de The process according to the invention relates in particular to the manufacture of composite ceramic materials as well as composite ceramic materials reinforced with fibers. It infiltrates a porous pre-ceramic part with a metal or
silicium, Le métal ou le silicium liquide s'y dépose dans les pores. silicon, Metal or liquid silicon is deposited there in the pores.
Dans le cas de l'infiltration par le silicium de pièces précéramiques à base de carbone, la réaction fait apparaître du carbure de silicium qui est la céramique proprement dite. Ce procédé est par exemple In the case of the infiltration by silicon of carbon-based preceramic parts, the reaction gives rise to silicon carbide which is the ceramic proper. This process is for example
décrit dans le document DE 44 38 455 Cl. described in document DE 44 38 455 Cl.
Ce procédé s'emploie en particulier lors de la fabrication de disques de frein céramiques. A cet égard, la fabrication de disques de frein ventilés de l'intérieur pose des problèmes. Il est très difficile d'obtenir des canaux de ventilation dans des disques céramiques massifs, du fait que le matériau est très réfractaire et difficile à usiner. Lors de l'obtention des canaux dans les pièces brutes précéramiques, des problèmes peuvent survenir parce que, selon les circonstances, les caractéristiques géométriques de la pièce et ses dimensions peuvent se trouver modifiées par suite de This process is used in particular during the manufacture of ceramic brake discs. In this regard, the production of internally ventilated brake discs poses problems. It is very difficult to obtain ventilation channels in solid ceramic discs, because the material is very refractory and difficult to machine. When obtaining channels in pre-ceramic blanks, problems may arise because, depending on the circumstances, the geometrical characteristics of the part and its dimensions may be changed as a result of
l'infiltration du bain de fusion.infiltration of the melt.
Le but de l'invention est donc de mettre à disposition un procédé du type mentionné ci-dessus avec lequel on puisse fabriquer des pièces céramiques présentant des structures internes, en The object of the invention is therefore to provide a method of the type mentioned above with which it is possible to manufacture ceramic pieces having internal structures,
particulier des canaux et analogues. especially channels and the like.
La solution réside dans le fait qu'à l'ébauche on ajoute au moins un noyau à teneur de métal ou de silicium qui, lors de l'infiltration du bain de fusion, s'emploie comme source de métal ou The solution lies in the fact that at the blank, at least one core containing a metal or silicon content is added which, during the infiltration of the melt, is used as a source of metal or
de silicium.of silicon.
Le procédé conforme à l'invention, avec lequel on infiltre d'un bain de fusion les pièces précéramiques en employant des noyaux à teneur de métal ou de silicium, les noyaux servant de source de métal au silicium, présente l'avantage que l'on peut fabriquer de la façon la plus simple, avec une haute précision de cote, des pièces The process according to the invention, with which the pre-ceramic parts are infiltrated by a fusion bath using cores with a metal or silicon content, the cores serving as a source of metal for the silicon, has the advantage that the we can manufacture in the simplest way, with high dimension accuracy, parts
composites à structure interne.composites with internal structure.
Une variante de la présente invention prévoit que l'on fabrique des pièces précéramiques ou des ébauches à structures internes, les noyaux étant insérés dans ces structures avant l'infiltration du bain de fusion. Une seconde forme de réalisation consiste en ce que l'on applique déjà lors du pressage de l'ébauche la structure interne, en particulier les canaux de ventilation, sous forme de noyaux à teneur de métal au silicium qui subsistent sur place jusqu'à l'infiltration du bain de fusion. On peut donc envisager aussi bien des noyaux servant de source de silicium pur que des noyaux opérant, par exemple lors de la fabrication de disques de frein ventilés, en tant que noyau de ventilation sous forme d'une garniture insérée en tant qu'outillage. Selon l'invention, on emploie de préférence des noyaux de métal ou de silicium techniquement purs. Une autre extension avantageuse prévoit d'employer un mélange de silicium et de nitrure de bore. Une troisième extension avantageuse consiste en l'emploi d'alliages, en particulier d'alliages silicium/fer ou d'alliages silicium/aluminium. On peut fabriquer ces noyaux par coulée ou pressage. La fabrication peut se faire sous gaz de protection. Un gaz de protection est nécessaire lors de la mise en fusion du silicium, avant la fabrication du noyau proprement dite. On peut fabriquer par coulée des noyaux de silicium allant de très pur à techniquement pur. Un procédé préféré de fabrication du noyau est le tir du noyau, tel qu'il s'applique par exemple lors de la fabrication du noyau de sable dans la technique de coulée. Des mélange silicium/nitrure de bore ou des alliages de silicium avec d'autres métaux peuvent être coulés, l'abaissement du point de fusion par rapport aux composants purs étant avantageux. On peut également les fabriquer A variant of the present invention provides for the production of pre-ceramic parts or blanks with internal structures, the cores being inserted into these structures before the infiltration of the molten bath. A second embodiment consists in applying the internal structure, in particular the ventilation channels, during the pressing of the blank, in the form of silicon metal content cores which remain in place until the 'infiltration of the melt. It is therefore possible to envisage both cores serving as a source of pure silicon as cores operating, for example during the manufacture of ventilated brake discs, as a ventilation core in the form of a lining inserted as tooling. According to the invention, preferably technically pure metal or silicon cores are used. Another advantageous extension provides for the use of a mixture of silicon and boron nitride. A third advantageous extension consists of the use of alloys, in particular silicon / iron alloys or silicon / aluminum alloys. These cores can be made by casting or pressing. Manufacturing can be done under protective gas. A shielding gas is necessary during the melting of the silicon, before the fabrication of the core itself. Silicon cores ranging from very pure to technically pure can be manufactured by casting. A preferred method of manufacturing the core is the firing of the core, as it applies for example during the manufacture of the sand core in the casting technique. Silicon / boron nitride mixtures or alloys of silicon with other metals can be cast, lowering the melting point relative to the pure components being advantageous. They can also be made
par extrusion ou par coulée sous pression. by extrusion or by die casting.
On peut également obtenir par fraisage, après le pressage de It can also be obtained by milling, after pressing
l'ébauche, les canaux à remplir de noyaux. the blank, the channels to be filled with cores.
Une autre extension avantageuse prévoit qu'une ébauche contenant des noyaux à teneur de métal ou de silicium soit obtenue sur une presse à enveloppe volante, à partir d'une masse à presser contenant un ou plusieurs noyaux. Les fibres contenues dans la masse à presser s'orientent alors le long du noyau à teneur de métal ou de silicium selon la direction de la force. La pièce céramique résultante présente les caractéristiques typiques d'une céramique, à savoir rigidité et résistance élevée à l'usure. Ces caractéristiques Another advantageous extension provides that a blank containing cores with a metal or silicon content is obtained on a flywheel press, from a pressing mass containing one or more cores. The fibers contained in the mass to be pressed are then oriented along the metal or silicon content core according to the direction of the force. The resulting ceramic part has the typical characteristics of a ceramic, namely rigidity and high resistance to wear. These characteristics
conviennent particulièrement bien pour des disques de frein. particularly suitable for brake discs.
On décrit en détail ci-dessous un exemple de réalisation de la présente invention à l'aide des dessins joints: - la figure la est une coupe schématique d'un dispositif de pressage d'une pièce précéramique formée contenant un noyau à teneur de silicium; avant (à droite) et après (à gauche) insertion du noyau la figure lb représente le dispositif de la figure la après le processus de pressage; la figure 2 est une coupe schématique d'une pièce précéramique formée que l'on peut obtenir avec le dispositif des figures la et lb. la figure 3 représente une autre forme de réalisation d'une An embodiment of the present invention is described in detail below with the aid of the accompanying drawings: FIG. 1a is a schematic section of a device for pressing a pre-ceramic formed part containing a core containing silicon ; before (on the right) and after (on the left) insertion of the core, figure lb represents the device of figure la after the pressing process; Figure 2 is a schematic sectional view of a pre-ceramic shaped part that can be obtained with the device of Figures la and lb. Figure 3 shows another embodiment of a
pièce précéramique formée contenant un noyau à teneur de silicium. pre-ceramic shaped part containing a silicon-containing core.
Pour fabriquer une pièce précéramique formée à partir d'une masse à presser, on peut employer un dispositif de pressage conventionnel. La masse à presser contient des fibres ou des faisceaux de matériau fibreux en fibres de silicium, de carbone, de bore et/ou à teneur d'azote avec un liant approprié pour la pyrolyse, d'autres liants, et charges. Les fibres ou les faisceaux de matériaux fibreux peuvent être imprégnés d'un liant convenant pour la pyrolyse et/ou revêtus de carbone pyrolytique. On presse cette masse pour fabriquer une ébauche. Puis on carbonise (on pyrolyse) l'ébauche sous vide ou sous gaz de protection pour fabriquer une pièce poreuse formée à teneur de carbone que l'on infiltre avec un To manufacture a pre-ceramic part formed from a mass to be pressed, a conventional pressing device can be used. The press material contains fibers or bundles of fibrous material made of silicon, carbon, boron and / or nitrogen fibers with a binder suitable for pyrolysis, other binders, and fillers. The fibers or bundles of fibrous materials can be impregnated with a binder suitable for pyrolysis and / or coated with pyrolytic carbon. This mass is pressed to make a blank. Then the blank is carbonized (pyrolyzed) under vacuum or under protective gas to manufacture a porous piece formed with carbon content which is infiltrated with a
bain de fusion de silicium.silicon fusion bath.
Le dispositif de pressage employé peut présenter des noyaux qui sont solidarisés avec la surface intérieure du dispositif de pressage. Mais les noyaux peuvent également être mobiles, par exemple être disposés hydrauliquement dans le dispositif de pressage. On enfiche les noyaux dans la masse à presser. On peut également introduire les noyaux dans le dispositif de pressage en les laissant libres. Après le pressage de l'ébauche, on extrait les noyaux, ce dont résulte une ébauche présentant des perçages de traversée. Dans ces perçages de traversée, on enfiche des noyaux qui sont constitués de silicium très pur ou techniquement pur, d'un mélange de silicium et de nitrure de bore ou d'un alliage contenant % de silicium et 40% de fer ou 60% de silicium et 40% d'aluminium. On carbonise et on silicifie ensuite, dans un procédé à The pressing device used may have cores which are integral with the interior surface of the pressing device. However, the cores can also be mobile, for example being arranged hydraulically in the pressing device. The cores are inserted into the mass to be pressed. The cores can also be introduced into the pressing device, leaving them free. After pressing the blank, the cores are extracted, which results in a blank with through holes. In these through holes, cores are plugged in which are made of very pure or technically pure silicon, a mixture of silicon and boron nitride or an alloy containing% silicon and 40% iron or 60% silicon and 40% aluminum. It is carbonized and then silicified, in a process with
une seule étape, les ébauches résultantes, garnies de ces noyaux. a single step, the resulting blanks, filled with these cores.
On peut par exemple couler les noyaux de silicium pur en les plaçant dans un moule, revêtu de nitrure de bore, que l'on remplit alors de silicium liquide. Après solidification, on peut enlever les noyaux finis. On peut par exemple fabriquer par tir de noyau ou par pressage isostatique des noyaux constitués d'un mélange de silicium et de nitrure de bore, éventuellement avec addition d'un liant. 1l est également possible de fabriquer une masse pâteuse de silicium, de nitrure de bore et d'un ou plusieurs liants et d'en obtenir des noyaux par extrusion, de façon comparable à l'extrusion des matières plastiques, connue en soit. On peut fabriquer des noyaux à partir d'un alliage, par exemple par mise en fusion ou pressage d'une poudre de métal avec une proportion d'environ 5 à 20% en poids de liant. En principe, il faudrait faire attention à ce que la teneur en silicium des noyaux suffise chaque fois pour une One can for example pour the cores of pure silicon by placing them in a mold, coated with boron nitride, which is then filled with liquid silicon. After solidification, the finished cores can be removed. One can for example manufacture by core firing or by isostatic pressing of the cores consisting of a mixture of silicon and boron nitride, optionally with the addition of a binder. It is also possible to manufacture a pasty mass of silicon, boron nitride and one or more binders and to obtain cores by extrusion, in a manner comparable to the extrusion of plastics, known per se. Cores can be made from an alloy, for example by melting or pressing a metal powder with a proportion of about 5 to 20% by weight of binder. In principle, care should be taken that the silicon content of the cores is sufficient for each
pénétration complète de la pièce précéramique formée à infiltrer. complete penetration of the pre-ceramic part formed to infiltrate.
L'homme de l'art peut calculer pour chaque cas particulier le degré de pureté ou la teneur en silicium puisque l'on peut aussi bien connaître le volume des canaux de l'ébauche que calculer le besoin en silicium pour l'infiltration par le bain de fusion. La fabrication du noyau peut se faire sous gaz de protection, la mise en fusion du Those skilled in the art can calculate for each particular case the degree of purity or the silicon content since it is possible to know the volume of the channels of the blank as well as to calculate the silicon requirement for infiltration by the fusion bath. The manufacturing of the core can be done under protective gas, the melting of the
silicium devant se faire sous gaz de protection. silicon to be done under shielding gas.
Ensuite, on soumet à une infiltration par bain de fusion, connue, l'ébauche munie des noyaux de silicium enfichés. Alors, le silicium contenu dans les noyaux fond et pénètre dans les pièces précéramiques formées poreuses, une transformation s'opérant avec le carbone contenu dans la pièce précéramique formée pour donner Next, the blank provided with plugged silicon cores is subjected to infiltration by known fusion bath. Then, the silicon contained in the cores melts and penetrates into the porous pre-ceramic parts, a transformation taking place with the carbon contained in the pre-ceramic part formed to give
le matériau céramique carbure de silicium. the silicon carbide ceramic material.
Les figures la et lb représentent un dispositif de pressage d'une pièce précéramique formée avec un noyau à teneur de silicium. Le dispositif 10 présente un poinçon supérieur 11 (figure lb) et un poinçon inférieur 12. Le poinçon inférieur 12 présente en outre un poinçon intérieur 13 qui peut se déplacer verticalement au moyen d'un dispositif de levage hydraulique 14. En outre le poinçon inférieur 12 est muni d'une " enveloppe volante " 15 qui peut également se déplacer verticalement au moyen d'un dispositif de Figures la and lb show a device for pressing a preceramic part formed with a core containing silicon. The device 10 has an upper punch 11 (FIG. 1b) and a lower punch 12. The lower punch 12 also has an inner punch 13 which can be moved vertically by means of a hydraulic lifting device 14. Furthermore, the lower punch 12 is provided with a "flying envelope" 15 which can also be moved vertically by means of a
levage hydraulique 16.hydraulic lifting 16.
On remplit de la masse à presser 30 (figure la à droite) l'espace intermédiaire situé entre la paroi intérieure de l'enveloppe volante 15 et la paroi intérieure du poinçon intérieur 13. Ensuite, on place dans le dispositif 10 un noyau en forme d'étoile 20 constitué de silicium ou de nitrure de bore ou d'un alliage à teneur de silicium. On peut fabriquer ce noyau en forme d'étoile 20 comme décrit ci-dessus. On place le noyau de façon que son bord extérieur a repose sur la face intérieure de l'enveloppe volante 15 et son bord intérieur 20b sur le poinçon intérieur 13. Le poinçon intérieur 13 et l'enveloppe volante 15 s'effacent alors un peu vers le bas le The intermediate mass located between the inner wall of the flying envelope 15 and the inner wall of the inner punch 13 is filled with pressing material 30 (FIG. 1a to the right). Next, a shaped core is placed in the device 10. of star 20 consisting of silicon or boron nitride or an alloy with a silicon content. This star-shaped core 20 can be made as described above. The core is placed so that its outer edge a rests on the inner face of the flying envelope 15 and its inner edge 20b on the inner punch 13. The inner punch 13 and the flying envelope 15 then fade a little towards down on
long de leur dispositif de levage 14 ou 16 (figure la, à gauche). along their lifting device 14 or 16 (figure la, on the left).
Aussi bien l'enveloppe volante 15 que le poinçon intérieur 13 Both the flying envelope 15 and the inner punch 13
peuvent être munis de réceptacles 15' ou 13' pour le noyau 20. may be provided with receptacles 15 ′ or 13 ′ for the core 20.
Ensuite, on pose une garniture annulaire 17 sur l'enveloppe volante 15 et sur le bord extérieur 20a du noyau 20 (figurerla à gauche). On remplit l'anneau 17 d'un complément de masse à presser 30. Puis le poinçon supérieur Il s'abaisse et la masse à presser 30 est pressée pour donner une pièce brute, l'enveloppe volante 15 et le poinçon intérieur 13 se déplaçant entièrement verticalement vers le bas Next, an annular lining 17 is placed on the flying envelope 15 and on the outer edge 20a of the core 20 (figured on the left). The ring 17 is filled with additional pressing mass 30. Then the upper punch It is lowered and the pressing mass 30 is pressed to give a blank, the flying envelope 15 and the inner punch 13 moving fully vertically down
(figure lb).(figure lb).
La pièce précéramique formée 40, finie, contenant le noyau en The pre-ceramic formed part 40, finished, containing the core in
forme d'étoile 20, est représentée schématiquement sur la figure 2. star shape 20, is shown diagrammatically in FIG. 2.
On la soumet ensuite de façon connue à une pyrolyse et à une infiltration par bain de fusion. Alors, le noyau en forme d'étoile 20 fond, le silicium pénètre dans les pores de la précéramique formée 40 et y forme du carbure de silicium. Il subsiste une pièce céramique présentant des perçages de traversée dont l'allure correspond avec une précision de cote élevée à celle du noyau en It is then subjected in a known manner to pyrolysis and to infiltration by a melt. Then, the star-shaped core 20 melts, the silicon penetrates into the pores of the pre-ceramic formed 40 and forms therein silicon carbide. There remains a ceramic part having through holes, the shape of which corresponds with a precision of dimension high to that of the core in
forme d'étoile.star shape.
La figure 3 représente une pièce formée 40' avec une variante ' du noyau en forme d'étoile de la figure 2 qui dans ce cas recouvre les bords de la pièce formée pressée 40. Cette variante présente un avantage car le noyau en forme d'étoile 20, 20' est relativement fragile. Dans le cas de la conception représentée sur la figure 3, le noyau en forme d'étoile 20' ne peut pas se déplacer à l'intérieur de la pièce précéramique formée 40' et reste donc FIG. 3 represents a formed part 40 ′ with a variant ′ of the star-shaped core of FIG. 2 which in this case covers the edges of the pressed formed part 40. This variant has an advantage because the core in the form of star 20, 20 'is relatively fragile. In the case of the design shown in FIG. 3, the star-shaped core 20 ′ cannot move inside the pre-ceramic formed part 40 ′ and therefore remains
fiablement intact pendant la totalité des processus de fabrication. reliably intact during the entire manufacturing process.
Claims (6)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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DE19834571A DE19834571C2 (en) | 1998-07-31 | 1998-07-31 | Process for the production of bodies from fiber-reinforced composite materials and use of the process |
Publications (2)
Publication Number | Publication Date |
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FR2781791A1 true FR2781791A1 (en) | 2000-02-04 |
FR2781791B1 FR2781791B1 (en) | 2002-01-25 |
Family
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FR9909854A Expired - Fee Related FR2781791B1 (en) | 1998-07-31 | 1999-07-29 | PROCESS FOR MANUFACTURING PARTS OF COMPOSITE MATERIALS REINFORCED WITH FIBERS |
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US (1) | US6328834B1 (en) |
DE (1) | DE19834571C2 (en) |
FR (1) | FR2781791B1 (en) |
GB (1) | GB2342102B (en) |
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US6255234B1 (en) * | 1997-01-30 | 2001-07-03 | Hitco Carbon Composites, Inc. | Ultra low friction carbon/carbon composites for extreme temperature applications |
US20050181209A1 (en) * | 1999-08-20 | 2005-08-18 | Karandikar Prashant G. | Nanotube-containing composite bodies, and methods for making same |
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DE10028532A1 (en) * | 2000-06-08 | 2001-12-13 | Bayerische Motoren Werke Ag | Vehicle brake disc, the friction ring and brake disc cup are made of different materials |
US6372165B1 (en) * | 2000-09-22 | 2002-04-16 | Praxair Technology, Inc. | Cold isopressing method |
AU2002212262A1 (en) * | 2000-10-18 | 2002-04-29 | Menzolit-Fibron Gmbh | Method for producing ceramic brake disks, with an insert in the green body before the pyrolysis |
DE10060566B4 (en) * | 2000-12-01 | 2005-09-08 | Dr.Ing.H.C. F. Porsche Ag | A friction body of silicon-infiltrated, carbon fiber-reinforced porous carbon, method for producing such a friction body and use of such a friction body |
EP1276704B1 (en) * | 2000-12-22 | 2003-10-29 | Freni Brembo S.p.A. | Process for the production of a braking band with venting passages and braking band obtained with said process |
JP5122723B2 (en) * | 2001-07-27 | 2013-01-16 | フレニ・ブレンボ エス・ピー・エー | Mold for molding and brake band manufacturing method for manufacturing a brake band having a ventilation duct in a composite material |
WO2003012310A1 (en) * | 2001-07-27 | 2003-02-13 | Freni Brembo S.P.A. | Process for the production of a braking band of a brake disk with ventilation ducts and a braking band produced by this process |
DE10148659C1 (en) * | 2001-10-02 | 2003-02-06 | Sgl Carbon Ag | Production of hollow bodies made from fiber-reinforced ceramic materials, used in brake and clutch disk production, comprises forming cores, forming green body from cores and carbonizing |
DE10148658C1 (en) * | 2001-10-02 | 2003-02-06 | Sgl Carbon Ag | Production of hollow bodies made from fiber-reinforced ceramic materials used in the production of brake and clutch disks comprises forming cores, forming a green body |
DE10164627C1 (en) * | 2001-12-31 | 2003-02-06 | Sgl Carbon Ag | Production of hollow bodies made from fiber-reinforced ceramic materials used in the production of brake and clutch disks comprises forming molding cores |
DE10209223A1 (en) * | 2002-03-04 | 2003-09-25 | Schunk Kohlenstofftechnik Gmbh | Process for the production of hollow bodies |
AU2002253522A1 (en) * | 2002-03-21 | 2003-10-08 | Freni Brembo S.P.A. | Disk brake caliper |
DE10222258A1 (en) * | 2002-03-22 | 2003-10-09 | Schunk Kohlenstofftechnik Gmbh | Composite ceramic body and method for producing such |
DE10223250B4 (en) * | 2002-05-22 | 2008-04-17 | Ing. Max Fuss Gmbh & Co. Kg | Device for the production of molded articles from fiber-reinforced ceramic materials |
US20040067316A1 (en) * | 2002-10-04 | 2004-04-08 | Paul Gray | Method for processing silicon-carbide materials using organic film formers |
DE10249283A1 (en) * | 2002-10-23 | 2004-05-19 | Daimlerchrysler Ag | Method of drilling holes in C / SiC composites |
DE10312159A1 (en) * | 2003-03-19 | 2004-09-30 | Sgl Carbon Ag | Device and method for pressing hollow bodies |
WO2004101249A1 (en) | 2003-05-14 | 2004-11-25 | Freni Brembo S.P.A. | Mould and method for the manufacture of a braking band of composite material, with ventilation ducts |
US20060062985A1 (en) * | 2004-04-26 | 2006-03-23 | Karandikar Prashant G | Nanotube-containing composite bodies, and methods for making same |
US7063870B2 (en) * | 2004-05-25 | 2006-06-20 | Honeywell International Inc. | Manufacture of functionally graded carbon-carbon composites |
US8017057B2 (en) | 2006-06-15 | 2011-09-13 | E. I. Du Pont De Nemours And Company | Method for making a pressed part with separations or voids |
DE102009050025A1 (en) * | 2009-10-21 | 2011-05-05 | Audi Ag | Ceramic brake disk for use in high speed brake system, has friction layers made of silicon and silicon carbide, where part of silicon carbide and/or carbon components of layers and/or carrier body is encapsulated in envelope |
GB2485673B (en) * | 2010-11-17 | 2017-11-15 | Meggitt Aerospace Ltd | Brake disc |
US20120186919A1 (en) * | 2011-01-26 | 2012-07-26 | GM Global Technology Operations LLC | Molded Components Having a Visible Designer Feature and/or Improved Operational Properties via a Porous Preform |
US10011043B2 (en) | 2012-04-27 | 2018-07-03 | General Electric Company | Method of producing an internal cavity in a ceramic matrix composite |
US10450235B2 (en) * | 2012-04-27 | 2019-10-22 | General Electric Company | Method of producing an internal cavity in a ceramic matrix composite and mandrel therefor |
EP3004559B1 (en) | 2013-05-29 | 2020-01-15 | General Electric Company | Method of forming a ceramic matrix composite component with cooling features |
US10597335B2 (en) | 2016-08-04 | 2020-03-24 | General Electric Company | Seal coats to prevent silicon loss during re-melt infiltration of Si containing composites |
DE102019215662A1 (en) * | 2019-10-11 | 2021-04-15 | Brembo Sgl Carbon Ceramic Brakes Gmbh | Internally ventilated rotor |
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-
1999
- 1999-07-29 FR FR9909854A patent/FR2781791B1/en not_active Expired - Fee Related
- 1999-07-29 GB GB9917854A patent/GB2342102B/en not_active Expired - Fee Related
- 1999-08-02 US US09/365,817 patent/US6328834B1/en not_active Expired - Lifetime
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DE4438455C1 (en) * | 1994-10-28 | 1996-05-02 | Deutsche Forsch Luft Raumfahrt | Process for producing a friction unit by infiltration of a porous carbon body with liquid silicon |
Also Published As
Publication number | Publication date |
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FR2781791B1 (en) | 2002-01-25 |
GB9917854D0 (en) | 1999-09-29 |
DE19834571C2 (en) | 2001-07-26 |
GB2342102A (en) | 2000-04-05 |
US6328834B1 (en) | 2001-12-11 |
DE19834571A1 (en) | 2000-02-03 |
GB2342102B (en) | 2001-03-14 |
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